NGM = NAM x GS ÷ TAS
NGM = NAM ± [wind component x Time (min)] ÷ 60
At first this question appears confusing. But let's start by determining the TAS at which the aircraft was flying:
Time to climb = 22 min
Ground distance covered = 66 nm (no wind)
- Speed = Distance ÷ Time (min) x 60 = 180 kt
- Ground speed = 180 kt - 35 kt = 145 kt
- NGM = NAM x GS ÷ TAS
NGM = 66 NM x 145 kt ÷ 180 kt
NGM = 53 NM
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